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Device and method for checking an aircraft landing gear shock absorber

  • US 9,978,189 B2
  • Filed: 04/23/2013
  • Issued: 05/22/2018
  • Est. Priority Date: 05/29/2012
  • Status: Active Grant
First Claim
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1. A method of checking whether a characteristic of the gas in an aircraft landing gear oleo is acceptable or not for an aircraft which is at rest, the oleo comprising an inner sliding tube having a known diameter and an outer covering in which the inner sliding tube slides, the exposed region of inner sliding tube being indicative of the amount of extension of the oleo, the method comprising the following steps:

  • capturing an image which depends on the amount of extension of the oleo with a hand-held electronic device, the image comprising said exposed region,measuring a width and height of the part of the image that defines the exposed region with the hand-held electronic device,deriving the amount of extension of the oleo with the hand-held device from the measured width and height of the part of the image that defines the exposed region and from the known value of the diameter of the inner sliding tube,obtaining an indication of the expected value of the characteristic of the gas in the oleo with the hand-held device from the amount of extension of the oleo,outputting with the hand-held electronic device an output in dependence on that indication of the expected value, providing a measure of the pressure in the landing gear obtained by other means, and generating an expected pressure from the measure of extension of the oleo and comparing the expected pressure to the pressure in the landing gear obtained by other means.

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